View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 51643U 26145.35206348 +.00000000 +00000-0 -19408-3 0 00007
2 51643 87.9164 10.3820 0002076 86.0356 274.1013 13.17648120 04
| Epoch (UTC): | 25 May 2026 08:26:58 |
| Eccentricity: | 0.0002076 |
| inclination: | 87.9164° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3820° |
| argument of perigee: | 86.0356° |
| revolutions per day: | 13.17648120 |
| mean anomaly at epoch: | 274.1013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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